contributor author | D. E. Paxson | |
contributor author | R. E. Mayle | |
date accessioned | 2017-05-08T23:36:56Z | |
date available | 2017-05-08T23:36:56Z | |
date copyright | July, 1991 | |
date issued | 1991 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28613#419_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109383 | |
description abstract | An investigation was conducted to study the unsteady effects of a moving wake as it passes over a laminar boundary layer in a stagnation region. Arguments are presented showing that in this region, the wake-induced unsteadiness may be treated, for the most part, as an inviscid, unsteady free stream, which impresses itself on the boundary layer flow. As a result, the boundary layer equations remain valid and, for relatively small oscillations, a solution to the equations may be obtained using standard perturbation techniques. A related experiment is then described and the results are examined in light of this analytical approach. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Laminar Boundary Layer Interaction With an Unsteady Passing Wake | |
type | Journal Paper | |
journal volume | 113 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2927891 | |
journal fristpage | 419 | |
journal lastpage | 427 | |
identifier eissn | 1528-8900 | |
keywords | Wakes | |
keywords | Boundary layers | |
keywords | Equations | |
keywords | Oscillations AND Flow (Dynamics) | |
tree | Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003 | |
contenttype | Fulltext | |